An evaluation of the design of the solar sail includes key areas such as structures, sail deployment, space environmental effects, materials, power systems, telemetry, communications, attitude control, thermal control, and trajectory analysis. Deployment and material constraints determine the basic structure of the sail, while the trajectory of the sail influences the choice of telemetry, communications, and attitude control systems. The thermal control system of the sail for the structures and electronics takes into account the effects of the space environment. Included also are a cost and weight estimate for the sail.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of a Solar Sail Mission to Mars


    Beteiligte:

    Erscheinungsdatum :

    1989-05-05


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design of a Solar Sail Mission to Mars

    Feaux, K. / Jordan, W. / Killough, G. et al. | NTRS | 1989


    Design of a Solar Sail Mission to Mars

    R. Eastridge / K. Funston / A. Okia et al. | NTIS | 1989


    Solar sail mission design

    Leipold, Manfred | TIBKAT | 2000


    Solar sail mission applications

    WRIGHT, J. / WARMKE, J. | AIAA | 1976


    Solar sail mission applications

    Wright, J. L. / Warmke, J. M. | NTRS | 1976